(20) and (25) near the top LH side of the engine. (Ref. Fig. 417A/TASK 71-51-43-991-320-A)
(9) Put the rubber supports in the line blocks (10) at station 174, line block (20) at station 176 and line block (25) at station 185.
(10) Make sure that the harness (5) is correctly installed on the engine.
(11) Close the line blocks (10), (20) and (25) and tighten the captive bolts.
(12) Put the harness (5) into the flip-lock clamps (30) and the rubber support of the line block (35) at station 191.
(13) If removed, put the rubber support in the line block (35).
(14) Close the line block (35) and tighten the captive bolt.
(15) Tighten the captive screws on the flip-lock clamps (30).
(16) Put the harness (5) into the rubber supports of the two line blocks
(35) at station 191 and station 199.
(Ref. Fig. 417A/TASK 71-51-43-991-320-A)
AFTER SPIB NO. CFM02255MW2
(Ref. Fig. 417A/TASK 71-51-43-991-320-A)
(17) Put the harness (5) into the rubber supports of the line blocks (10) near the top LH side of the engine. (Ref. Fig. 417A/TASK 71-51-43-991-320-A)
(18) Put the rubber supports in the line blocks (10) at station 174.
(19) Make sure that the harness (5) is correctly installed on the engine.
F 『R EEFF : 062-099, 103-149, 151-199, 203-299, E Page B41471-51-43
E E301-399, 401-499, Aug 01/05 E E ECES E E 56-5B E E E (20) Close the line blocks (10) and tighten the captive bolts.
F 『
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E E
(21) Install the bolt and clamps (22) that attach the harness (5) at
station 176.
(22) Install the bolt and clamps (27) that attach the harness (5) to the bracket at station 185.
(23) Install the nuts, bolts and clamps (32) that attach the harness (5) to the brackets at station 191.
(24) Install the harness (5) into the flip-lock clamp (30) at station 191 and tighten the captive bolt.
(25) Install the bolt and clamps (37) that attach the harness (5) to the bracket at station 191.
(26) Install the bolt, clamps and anti-rotation lug (38) that attach the harness (5) to the bracket at station 199. (Ref. Fig. 417A/TASK 71-51-43-991-320-A)
(27) Put the harness (5) into the rubber supports of the line block (35) at station 191 and the two line blocks (50) at station 199.
(28) If removed, put the rubber supports in the line blocks (35) and (50).
(29) Make sure that the harness (5) is correctly installed on the engine.
(30) Close the line blocks (35) and (50) and tighten the captive bolts. END SPIB NO.CFM02255MW1
(31) Put the clamp (85) on the harness (5). Attach the clamp (85) to the bracket at station 199 with the bolt (70), the washer (75), and the nut (80).
(32) Put the clamp (85) on the harness (5). Attach the clamp (85) to the bracket at station 191 and station 199 with the bolt (90).
(33) Make sure that the harness (5) is correctly installed on the engine.
(34) Put the clamps (55) on the harness (5). Attach the clamps to the brackets at station 199 with the bolts (40).
(35) Put the clamp (55) on the harness (5). Attach the clamp to the
bracket on tube flange with the bolt (40).
F 『R EEFF : 062-099, 103-149, 151-199, 203-299, E Page B41571-51-43
E E301-399, 401-499, Aug 01/05 E E ECES E
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E 56-5B E
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(36) Put the clamp (55) on the harness (5). Attach the clamp to the bracket at fuel control flange with the bolt (40).
(37) Put the clamp (55) on the harness (5). Attach the clamp to the bracket on gearbox with the bolts (40) and nut (65).
(38) TORQUE the bolts (40) and (60) and the nut (65) to between 20 and 25 lbf.in (0.22 and 0.28 m.daN).
(39) Connect the electrical connector 4000WD2-A to the fire detector loop
B.
(40) Examine the harness installation and make sure that the flip-lock clamps and the line blocks are installed correctly.
**ON A/C ALL
Subtask 71-51-43-865-088
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 3DA1, 3DA2, 3DA3, 4DA1, 4DA2, 4DA3, 5DA1, 5DA2, 5DA3, 1DB1, 1DB2, 4DG1, 4DG2, 1JH, 3801GX, 3802GX, 3803GX, 7TU, 2RK, 4RK FOR 1000EM1 2KS1, 4KS1, 2JH1, 3JH1, 1WE1, 2WE1, 7WD1, 8WD1, 2XU1 FOR 1000EM2 2KS2, 4KS2, 2JH2, 3JH2, 1WE2, 2WE2, 7WD2, 8WD2, 2XU2
Subtask 71-51-43-861-059
C. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002)
Subtask 71-51-43-860-080
D. Do the EIS start procedure (for the lower display of the ECAM system only). (Ref. TASK 31-60-00-860-001).
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本文链接地址：A320飞机维护手册 AMM 动力装置 POWER PLANT 2(71)
